View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20203U 26140.54198257 +.00000000 +00000-0 +00000-0 0 00004
2 20203 14.7089 4.2850 0011716 16.7519 153.7178 0.99116875 00
| Epoch (UTC): | 20 May 2026 13:00:27 |
| Eccentricity: | 0.0011716 |
| inclination: | 14.7089° |
| perigee height: | 36064 km |
| apogee height: | 36163 km |
| right ascension of ascending node: | 4.2850° |
| argument of perigee: | 16.7519° |
| revolutions per day: | 0.99116875 |
| mean anomaly at epoch: | 153.7178° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|